View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 37463U 99025EJH 23339.29105843 .00014429 00000-0 21800-2 0 9993
2 37463 98.7510 278.2452 0084279 158.2839 202.1973 14.71980748566102
| Epoch (UTC): | 05 December 2023 06:59:07 |
| Eccentricity: | 0.0084279 |
| inclination: | 98.7510° |
| perigee height: | 595 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 278.2452° |
| argument of perigee: | 158.2839° |
| revolutions per day: | 14.71980748 |
| mean anomaly at epoch: | 202.1973° |
| orbit number at epoch: | 56610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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